Detail publikace

Buckling and Failure of Composite Web

JURAČKA, J.

Anglický název

Buckling and Failure of Composite Web

Typ

Článek recenzovaný mimo WoS a Scopus

Jazyk

en

Originální abstrakt

The paper describes the strength analysis of composite structures of aircraft wings by FEM and its experimental verification. Modelling and experimental work were done at a wing of all-composite UL aircrafts UFM-10 Samba and TL-2000 Carbon Sting. The first part of the paper demonstrates the creation of the individual structure models of both wings and their analysis followed by the description of a real wing test. The paper compares the computational outputs with the results obtained by experimental measuring done during the tests. The conclusions show the correspondence of the experimental results with the FEM analysis.

Klíčová slova anglicky

FEM, modelling, composite structure, composites, wing

Vydáno

2003-01-01

Místo

Vilnius

ISSN

1648-7788

Časopis

Aviation

Ročník

VII

Číslo

1

Strany od–do

36–39

Počet stran

4

BIBTEX


@article{BUT44395,
  author="Jaroslav {Juračka}",
  title="Buckling and Failure of Composite Web",
  journal="Aviation",
  year="2003",
  volume="VII",
  number="1",
  pages="36--39",
  issn="1648-7788"
}